航空精密制造技术
航空精密製造技術
항공정밀제조기술
AVIATION PRECISION MANUFACTURING TECHNOLOGY
2014年
2期
42-44
,共3页
馈电缝%刀具变形%零件变形%高速切削
饋電縫%刀具變形%零件變形%高速切削
궤전봉%도구변형%령건변형%고속절삭
feed sewing%cutting tool deformation%part deformation%high speed cutting
通过对雷达天线馈电腔体中馈电缝的加工工艺理论分析及试验,结果表明,在加工条件允许的范围内,尽可能选用直径较大的刀具,缩短刀长,采用高转速、小切削量、快进给的切削方式,运用粗精加工分开的工艺路线,最终达到零件的设计要求。
通過對雷達天線饋電腔體中饋電縫的加工工藝理論分析及試驗,結果錶明,在加工條件允許的範圍內,儘可能選用直徑較大的刀具,縮短刀長,採用高轉速、小切削量、快進給的切削方式,運用粗精加工分開的工藝路線,最終達到零件的設計要求。
통과대뢰체천선궤전강체중궤전봉적가공공예이론분석급시험,결과표명,재가공조건윤허적범위내,진가능선용직경교대적도구,축단도장,채용고전속、소절삭량、쾌진급적절삭방식,운용조정가공분개적공예로선,최종체도령건적설계요구。
The theoretical analysis and test of machining technology for feed sewing in the feed cavity of radar antenna was made. The result shows that when the processing condition permits, tool having a large diameter should be chosen as much as possible, the length of tool should be shortened, the cutting way with a high speed, small cutting volume and quick feed should be used, and the technical method that has separated rough and finishing processing should be adopted.